EP2104886A4 - Flight control system - Google Patents
Flight control systemInfo
- Publication number
- EP2104886A4 EP2104886A4 EP07845466.7A EP07845466A EP2104886A4 EP 2104886 A4 EP2104886 A4 EP 2104886A4 EP 07845466 A EP07845466 A EP 07845466A EP 2104886 A4 EP2104886 A4 EP 2104886A4
- Authority
- EP
- European Patent Office
- Prior art keywords
- control system
- flight control
- flight
- control
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Granted
Links
- RZVHIXYEVGDQDX-UHFFFAOYSA-N 9,10-anthraquinone Chemical compound C1=CC=C2C(=O)C3=CC=CC=C3C(=O)C2=C1 RZVHIXYEVGDQDX-UHFFFAOYSA-N 0.000 title 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C9/00—Adjustable control surfaces or members, e.g. rudders
- B64C9/32—Air braking surfaces
-
- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
- G05D1/00—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
- G05D1/04—Control of altitude or depth
- G05D1/06—Rate of change of altitude or depth
- G05D1/0607—Rate of change of altitude or depth specially adapted for aircraft
- G05D1/0653—Rate of change of altitude or depth specially adapted for aircraft during a phase of take-off or landing
- G05D1/0676—Rate of change of altitude or depth specially adapted for aircraft during a phase of take-off or landing specially adapted for landing
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C19/00—Aircraft control not otherwise provided for
- B64C19/02—Conjoint controls
-
- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
- G05D1/00—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
- G05D1/04—Control of altitude or depth
- G05D1/06—Rate of change of altitude or depth
- G05D1/0607—Rate of change of altitude or depth specially adapted for aircraft
-
- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
- G05D1/00—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
- G05D1/08—Control of attitude, i.e. control of roll, pitch, or yaw
-
- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
- G05D1/00—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
- G05D1/08—Control of attitude, i.e. control of roll, pitch, or yaw
- G05D1/0808—Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Automation & Control Theory (AREA)
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
- Traffic Control Systems (AREA)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB0624700A GB2444742B (en) | 2006-12-11 | 2006-12-11 | Flight Control System |
PCT/BR2007/000340 WO2008070944A2 (en) | 2006-12-11 | 2007-12-11 | Flight control system |
Publications (3)
Publication Number | Publication Date |
---|---|
EP2104886A2 EP2104886A2 (en) | 2009-09-30 |
EP2104886A4 true EP2104886A4 (en) | 2013-07-24 |
EP2104886B1 EP2104886B1 (en) | 2017-11-22 |
Family
ID=37711920
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP07845466.7A Active EP2104886B1 (en) | 2006-12-11 | 2007-12-11 | Flight control system |
Country Status (6)
Country | Link |
---|---|
US (1) | US9405295B2 (en) |
EP (1) | EP2104886B1 (en) |
BR (1) | BRPI0709485B1 (en) |
CA (1) | CA2670918C (en) |
GB (1) | GB2444742B (en) |
WO (1) | WO2008070944A2 (en) |
Families Citing this family (17)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2942612B1 (en) * | 2009-03-02 | 2012-09-28 | Airbus France | METHOD AND DEVICE FOR AUTOMATIC OPTIMIZATION ON THE GROUND OF THE AERODYNAMIC CONFIGURATION OF AN AIRCRAFT |
RU2443602C2 (en) * | 2009-11-26 | 2012-02-27 | Московский государственный университет приборостроения и информатики | Aircraft pitch automatic control system |
FR2956512B1 (en) * | 2010-02-16 | 2012-03-09 | Airbus Operations Sas | METHOD AND DEVICE FOR AUTOMATIC PROTECTION OF AN AIRCRAFT AGAINST AN EXCESSIVE DESCENT RATE. |
US8666567B2 (en) | 2011-03-31 | 2014-03-04 | Honeywell International Inc. | Systems and methods for controlling the speed of an aircraft |
FR2980610B1 (en) * | 2011-09-23 | 2014-07-11 | Airbus Operations Sas | METHOD AND DEVICE FOR PREDICTING FUEL CONSUMPTION ON AN AIRCRAFT. |
US8606437B2 (en) * | 2011-11-28 | 2013-12-10 | Embraer S.A. | Flight control system mode and method providing aircraft speed control through the usage of momentary on-off control |
US8781653B2 (en) * | 2012-01-11 | 2014-07-15 | The Boeing Company | Quiet landing attitude modifier for airplane |
US9153139B2 (en) * | 2012-12-21 | 2015-10-06 | Embraer S.A. | Steep approach performance improvements and optimization |
JP6097596B2 (en) * | 2013-02-28 | 2017-03-15 | 三菱航空機株式会社 | Grand spoiler drive system and aircraft |
FR3010696B1 (en) * | 2013-09-13 | 2015-10-09 | Airbus Operations Sas | METHOD AND SYSTEM FOR CONTROLLING FLIGHT OF AN AIRCRAFT |
US20150321748A1 (en) * | 2014-05-08 | 2015-11-12 | Honeywell International Inc. | Speed brake alerting system and method |
CN105094141A (en) * | 2014-05-20 | 2015-11-25 | 哈尔滨飞机工业集团有限责任公司 | Digital autopilot system of lightweight fixed-wing aircraft |
US9821903B2 (en) | 2014-07-14 | 2017-11-21 | The Boeing Company | Closed loop control of aircraft control surfaces |
CN105955288B (en) * | 2016-07-15 | 2021-04-09 | 北京远度互联科技有限公司 | Aircraft positioning and control method and system |
US10228692B2 (en) | 2017-03-27 | 2019-03-12 | Gulfstream Aerospace Corporation | Aircraft flight envelope protection and recovery autopilot |
CN110162064A (en) * | 2019-06-14 | 2019-08-23 | 湖南汽车工程职业学院 | A kind of automatic Pilot positioning and control system for tour bus |
US11679865B2 (en) | 2021-06-21 | 2023-06-20 | Honeywell International Inc. | Aircraft yoke interference detection system and method |
Citations (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3589648A (en) * | 1969-01-02 | 1971-06-29 | Lockheed Aircraft Corp | Means for controlling the vertical path of an aircraft |
US4363098A (en) * | 1980-06-24 | 1982-12-07 | The Boeing Company | Electric command spoiler system |
US5337982A (en) * | 1991-10-10 | 1994-08-16 | Honeywell Inc. | Apparatus and method for controlling the vertical profile of an aircraft |
EP0708393A1 (en) * | 1994-10-19 | 1996-04-24 | Honeywell Inc. | Self-adaptive limiter for automatic control of approach and landing |
US5823479A (en) * | 1996-05-20 | 1998-10-20 | The Boeing Company | Landing attitude modifier for airplane |
US6062513A (en) * | 1998-09-14 | 2000-05-16 | The Boeing Company | Total energy based flight control system |
WO2006016070A1 (en) * | 2004-07-16 | 2006-02-16 | Airbus France | Method and device for improving maneuverability of an aircraft during approach phases before landing followed by flare-out |
Family Cites Families (17)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3040316A (en) * | 1959-06-22 | 1962-06-19 | Delaine C Sather | Limiting circuit for an aircraft control system |
US3252675A (en) * | 1963-10-18 | 1966-05-24 | Sperry Rand Corp | Monitoring apparatus for aircraft control system |
US3870253A (en) * | 1971-07-21 | 1975-03-11 | Mc Donnell Douglas Corp | Aircraft vectored flight control means |
US3738594A (en) | 1971-08-16 | 1973-06-12 | Mc Donnell Douglas Corp | Lift control mechanism |
US3774869A (en) | 1972-03-07 | 1973-11-27 | K Harmon | Combined throttle spoiler actuator for aircraft |
US3850388A (en) | 1972-03-23 | 1974-11-26 | Nasa | Integrated lift/drag controller for aircraft |
US4106730A (en) * | 1976-10-01 | 1978-08-15 | The Boeing Company | Engine out control system for STOL aircraft |
US4261537A (en) * | 1979-02-28 | 1981-04-14 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Velocity vector control system augmented with direct lift control |
US4266743A (en) * | 1979-02-28 | 1981-05-12 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Pitch attitude stabilization system utilizing engine pressure ratio feedback signals |
US4489907A (en) | 1982-06-23 | 1984-12-25 | Precise Flight, Inc. | Selectively integrated throttle spoiler actuator for aircraft |
US4849900A (en) * | 1986-05-02 | 1989-07-18 | The Boeing Company | Flight control system and method |
FR2661149B1 (en) | 1990-04-24 | 1992-08-14 | Aerospatiale | SYSTEM FOR THE PILOTAGE OF AN AIRPLANE IN TANGAGE. |
FR2719548B1 (en) * | 1994-05-03 | 1996-07-05 | Aerospatiale | Transport plane with front tail. |
US6246929B1 (en) * | 1999-06-16 | 2001-06-12 | Lockheed Martin Corporation | Enhanced stall and recovery control system |
DE10160315A1 (en) * | 2001-12-07 | 2003-11-13 | Airbus Gmbh | Device for the approach control of an aircraft |
US6885917B2 (en) * | 2002-11-07 | 2005-04-26 | The Boeing Company | Enhanced flight control systems and methods for a jet powered tri-mode aircraft |
FR2859174B1 (en) * | 2003-08-26 | 2006-03-10 | Airbus France | METHOD AND DEVICE FOR CONTROLLING THE PLATE OF AN AIRCRAFT |
-
2006
- 2006-12-11 GB GB0624700A patent/GB2444742B/en active Active
-
2007
- 2007-12-11 WO PCT/BR2007/000340 patent/WO2008070944A2/en active Application Filing
- 2007-12-11 CA CA2670918A patent/CA2670918C/en active Active
- 2007-12-11 US US12/518,361 patent/US9405295B2/en active Active
- 2007-12-11 EP EP07845466.7A patent/EP2104886B1/en active Active
- 2007-12-11 BR BRPI0709485A patent/BRPI0709485B1/en active IP Right Grant
Patent Citations (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3589648A (en) * | 1969-01-02 | 1971-06-29 | Lockheed Aircraft Corp | Means for controlling the vertical path of an aircraft |
US4363098A (en) * | 1980-06-24 | 1982-12-07 | The Boeing Company | Electric command spoiler system |
US5337982A (en) * | 1991-10-10 | 1994-08-16 | Honeywell Inc. | Apparatus and method for controlling the vertical profile of an aircraft |
EP0708393A1 (en) * | 1994-10-19 | 1996-04-24 | Honeywell Inc. | Self-adaptive limiter for automatic control of approach and landing |
US5823479A (en) * | 1996-05-20 | 1998-10-20 | The Boeing Company | Landing attitude modifier for airplane |
US6062513A (en) * | 1998-09-14 | 2000-05-16 | The Boeing Company | Total energy based flight control system |
WO2006016070A1 (en) * | 2004-07-16 | 2006-02-16 | Airbus France | Method and device for improving maneuverability of an aircraft during approach phases before landing followed by flare-out |
Non-Patent Citations (1)
Title |
---|
See also references of WO2008070944A2 * |
Also Published As
Publication number | Publication date |
---|---|
GB0624700D0 (en) | 2007-01-17 |
BRPI0709485A8 (en) | 2018-05-02 |
CA2670918A1 (en) | 2008-06-19 |
CA2670918C (en) | 2016-05-03 |
GB2444742A (en) | 2008-06-18 |
WO2008070944A2 (en) | 2008-06-19 |
US9405295B2 (en) | 2016-08-02 |
EP2104886B1 (en) | 2017-11-22 |
US20100217460A1 (en) | 2010-08-26 |
BRPI0709485A2 (en) | 2011-07-19 |
WO2008070944A3 (en) | 2009-04-02 |
BRPI0709485B1 (en) | 2019-01-29 |
GB2444742B (en) | 2011-06-08 |
EP2104886A2 (en) | 2009-09-30 |
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